• DocumentCode
    943183
  • Title

    A Reliability Analysis of Recoverable Missiles

  • Author

    Broeder, George G den, Jr. ; Kane, William E.

  • Author_Institution
    Lockheed Missile Systems Division, Palo Alto, California
  • fYear
    1959
  • fDate
    6/1/1959 12:00:00 AM
  • Firstpage
    34
  • Lastpage
    40
  • Abstract
    -Missiles with built-in recoverability features have been of interest to most missile firms and many related firms for some time. In order to evaluate the adequacy of recoverable missile performance, it is frequently necessary to answer such questions as, ``With what probability will m such missiles yield a total of N or more successful flights?´´ or, ``How many missiles should be allocated to a test program in which N or more successful flights must be realized with probability Q?´´ Answers to these questions are obtained in terms of three basic reliability characteristics: 1. probability of a successful flight, 2. probability of recovering after a successful flight, and 3. probability of recovering after an unsuccessful flight. In addition, a decision rule is derived for selecting the ``best´´ reliability program.
  • Keywords
    History; Missiles; Probability distribution; Testing; Tin; Vehicles;
  • fLanguage
    English
  • Journal_Title
    Reliability and Quality Control, IRE Transactions on
  • Publisher
    ieee
  • ISSN
    0097-4552
  • Type

    jour

  • DOI
    10.1109/IRE-PGRQC.1959.5007207
  • Filename
    5007207